Collaborative Optimization based on approximate technology is applied to plane wing design.
将本文研究的基于近似技术的协同优化方法应用在机翼设计中。
Wi th the dynamic analysis of J8-II plane wing, the numerical experiments in PAR95 show that the algorithm is very effective.
在大规模并行计算机PAR95上结合J8- II机翼的动力特性问题对该算法作了数值试验，结果说明所给算法是非常有效的。
Wi th the dynamic analysis of J8-II plane wing, the numerical experiments in PAR95 show that the algorithm is very effective.
在大规模并行计算机PAR95上结合J8- II机翼的动力特性问题对该算法作了数值试验，结果说明所给算法是非常有效的。
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